Experimental Approach to Improve Ion Thruster Performance: Part 1 Effects of the Propellant Delivery Method
スポンサーリンク
概要
著者
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TAKEGAHARA Haruki
Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology
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Takegahara Haruki
Department Of Aerospace Engineering Tokyo Metropolitan Institute Of Technology
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OKAWA Yasushi
Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology
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Okawa Y
Department Of Aerospace Engineering Tokyo Metropolitan Institute Of Technology
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Okawa Yasushi
Department Of Aerospace Engineering Tokyo Metropolitan Institute Of Technology
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Takegahara Haruki
Department of Aerospace Engineering
関連論文
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- Study on C_60 Application to Ion Thruster : Fundmental Processes of Ion Production and Extraction
- Experimental Approach to Improve Ion Thruster Performance: Part 2 Effects of Magnetic Field
- Experimental Approach to Improve Ion Thruster Performance: Part 1 Effects of the Propellant Delivery Method
- Guided Modes of Electron Wave in a Si-Quantum Wire
- Numerical Study of Beam Extraction Phenomena in an Ion Thruster
- Feasibility Study on C 60 Plasma Application to Ion Thruster